WO2012022946A1 - Improvements in damped hinge assemblies - Google Patents
Improvements in damped hinge assemblies Download PDFInfo
- Publication number
- WO2012022946A1 WO2012022946A1 PCT/GB2011/001249 GB2011001249W WO2012022946A1 WO 2012022946 A1 WO2012022946 A1 WO 2012022946A1 GB 2011001249 W GB2011001249 W GB 2011001249W WO 2012022946 A1 WO2012022946 A1 WO 2012022946A1
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- WO
- WIPO (PCT)
- Prior art keywords
- damper
- hinge assembly
- hinge
- assembly
- damped
- Prior art date
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- 230000000712 assembly Effects 0.000 title description 7
- 238000000429 assembly Methods 0.000 title description 7
- 238000006073 displacement reaction Methods 0.000 claims abstract description 13
- 238000013016 damping Methods 0.000 claims description 16
- 230000006835 compression Effects 0.000 claims description 12
- 238000007906 compression Methods 0.000 claims description 12
- 230000000630 rising effect Effects 0.000 claims description 2
- 230000007246 mechanism Effects 0.000 description 7
- 230000000694 effects Effects 0.000 description 3
- 230000005484 gravity Effects 0.000 description 3
- 230000009471 action Effects 0.000 description 2
- 230000008602 contraction Effects 0.000 description 2
- 229920001296 polysiloxane Polymers 0.000 description 2
- 230000000284 resting effect Effects 0.000 description 2
- 230000003190 augmentative effect Effects 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000009977 dual effect Effects 0.000 description 1
- 238000005755 formation reaction Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 239000002991 molded plastic Substances 0.000 description 1
- 230000004044 response Effects 0.000 description 1
- 230000000717 retained effect Effects 0.000 description 1
Classifications
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- A—HUMAN NECESSITIES
- A47—FURNITURE; DOMESTIC ARTICLES OR APPLIANCES; COFFEE MILLS; SPICE MILLS; SUCTION CLEANERS IN GENERAL
- A47K—SANITARY EQUIPMENT NOT OTHERWISE PROVIDED FOR; TOILET ACCESSORIES
- A47K13/00—Seats or covers for all kinds of closets
- A47K13/12—Hinges
-
- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05F—DEVICES FOR MOVING WINGS INTO OPEN OR CLOSED POSITION; CHECKS FOR WINGS; WING FITTINGS NOT OTHERWISE PROVIDED FOR, CONCERNED WITH THE FUNCTIONING OF THE WING
- E05F3/00—Closers or openers with braking devices, e.g. checks; Construction of pneumatic or liquid braking devices
- E05F3/20—Closers or openers with braking devices, e.g. checks; Construction of pneumatic or liquid braking devices in hinges
-
- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05Y—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES E05D AND E05F, RELATING TO CONSTRUCTION ELEMENTS, ELECTRIC CONTROL, POWER SUPPLY, POWER SIGNAL OR TRANSMISSION, USER INTERFACES, MOUNTING OR COUPLING, DETAILS, ACCESSORIES, AUXILIARY OPERATIONS NOT OTHERWISE PROVIDED FOR, APPLICATION THEREOF
- E05Y2999/00—Subject-matter not otherwise provided for in this subclass
Definitions
- This invention relates to damped hinge assemblies and more particularly, though not exclusively, to damped hinge assemblies for mounting elements such as lids, seats and doors.
- the invention provides a damped hinge assembly for mounting a first member for pivotal movement relative to a second member about an axis of rotation, the assembly comprising a linear damper, means mounting the damper with its longitudinal axis parallel to the hinge axis, and camming means for converting pivotal movement of the first member in at least one direction of rotation into linear displacement of the damper to cause the damper to produce a damped resistive force to counter said pivotal movement of the first member, wherein the longitudinal axis of the damper is arranged to be coincident with the hinge axis.
- Figure 1 shows a first form of damped hinge assembly according to the invention (shown partly cut-away to reveal detail),
- FIG. 1 is a detail view of the drive mechanism of the assembly of Figure 1
- FIG. 3 is an exploded view of the Figure 2 detail
- Figure 4 shows a second form of damped hinge assembly according to the invention (shown partly cut-away to reveal detail), Figures 5 and 6 show in partly cut-away detail the damping unit of the assembly of Figure 4, and
- Firgure 7 shows in partly cut-away detail an alternative form of damping unit for the assembly of Figure 4.
- the damped hinge assembly seen in Figure 1 is for use on a lavatory seat 11.
- the seat 11 comprises a lid member 12 and a seat member 13, both of which are pivotally mounted onto the lavatory 14 by means of a hinge mounted on a block 22 (shown partly cut away in the drawings).
- the block 22 is anchored to the lavatory 14 by means of the usual spaced apart threaded fasteners 16.
- the arrangement enables both the lid and seat members 12, 13 to be pivotable between a lower, generally horizontal position resting on the lavatory 14 and a raised position, generally slightly beyond vertical and resting against a cistern or wall or the like.
- the assembly is arranged to provide a damped resistive force to counter the pivotal movement of both the lid and seat members 12, 13 as they move under gravity from their raised position to their lowered position. This is intended to avoid possible damage that could otherwise occur if the lid and/or seat members were accidentally allowed to fall freely onto the lavatory.
- the assembly comprises a damper 17, which is conveniently located in the space between the hinge block mounting fasteners 16.
- the damper 17 here is a linear damper of the piston and cylinder variety, with a piston (not shown) connected to a piston rod 18 and acting within a cylinder 19 on a damping medium (not shown) such as silicone (see Figure 3).
- the damper 17 incorporates a spring (not shown) arranged to bias the piston rod 18 towards its extended position.
- the damper 17 is designed here to provide the damped resistive force-to the lid and/or seat members 12, 13 in response to its axial compression. However, the damper 17 provides no damped resistance upon its axial extension.
- the damper 17 is mounted on the block 22 and arranged with its longitudinal axis coincident with the pivotal axis 20 of the assembly.
- the damper 17 is captured in this position between two spaced apart end caps 21a, 21b.
- Each end cap 21a, 21b is generally cylindrical and has an axially extending rib 23a, 23b which engages in a groove 24 in the block 22.
- the groove 24 extends parallel to the pivotal axis 20 of the assembly.
- the arrangement means that the two end caps 21a, 21b are both capable of linear movement parallel to the pivotal axis 20 of the assembly (both towards and away from each other), but are prevented from rotating relative to the block 22.
- movement of the end caps 21a, 21b towards each other will cause axial compression of the damper 17, whilst movement of the end caps 21a, 21b away from each other will allow axial extension of the damper, under the influence of its spring.
- the lid and seat members 12, 13 each have a respective driving element 30a, 30b associated therewith.
- Each driving element 30a, 30b is rotatably mounted on the assembly by means of a spindle 3 la, 3 lb journalled in a bore in the block 22.
- the axis of rotation of the spindles 31a, 31b is coincident with the pivotal axis 20 of the assembly.
- Each driving element 30a, 30b is arranged to be keyed to its respective lid/seat member 12, 13 so as to rotate therewith.
- the spindle 31a of its respective driving element 30a is provided with flats 37a and fits in a flatted hole 36 in the hinge part of the lid member.
- the arrangement means that whenever the lid member 12 is pivoted, the spindle 31a and hence its associated driving element 30a will likewise be driven to rotate.
- the spindle 31b is provided with flats 37b and fits in a flatted hole in the hinge part of the seat member 13 so that whenever the seat member is pivoted, the spindle 31b and hence its associated driving element 30b will likewise be driven to rotate.
- Each driving element 30a, 30b has circumferentially extending ramped surfaces 34a, 34b on its axially inwardly facing end.
- the ramped surfaces are provided on their elements as diametrically opposed pairs, as can be seen in the case of the driving element 30b for the seat member in Figure 3.
- Each of these ramped surfaces 34a, 34b is engaged by a respective nib 35a, 35b on the end caps 21a, 21b (again provided as diametrically opposed pairs).
- the nibs 35a, 35b will be biassed into engagement with their respective ramped surfaces 34a, 34b by the action of the spring in the damper 17.
- this arrangement means that when either of the driving elements 30a, 30b rotates, its ramped surface 34a, 34b will act on the respective nib 35a, 35b to cause longitudinal displacement of its respective end cap 21a, 21b.
- the ramped surfaces 34a, 34b and nibs 35a, 35b thus act in the manner of a cam and cam follower, translating rotational movement into linear movement.
- the rotational movement of the lid and/or seat members 12, 13 is thus translated by this motion converting mechanism into linear displacement (extension or compression) of the damper 17.
- the assembly is seen in its condition when the lid member is in its raised position, whilst the seat member is in its lower position.
- the driving element 30b associated with the seat member has been rotated in the direction of arrow A as the seat member has lowered. This has driven its associated end cap 21b in the direction of arrow B by the camming action of the ramped surface 34b on the nib 35b. Movement of the end cap 21b in this manner has caused compression of the damper 17, thereby imparting a damped resistive force to the lowering movement of the seat member. It will be understood that the manner of engagement of the nibs
- the ramped surfaces 34a, 34b on the driving elements 30a, 30b are configured such that pivotal movement of the lid and/or seat members 12, 13 in their lowering direction will cause linear movement of the end caps 21a, 21b in a direction towards each other. The effect of this will be to cause axial compression of the damper 17. Axial compression of the damper 17 will in turn create a resistive damping force which is transmitted back through the drive mechanism to .the lid and/or seat members 12, 13 and hence attenuate their closing movement.
- damper 17 will be actuated to provide a damped resistive force to the closing movement of the lid or seat members 12, 13 moving singly, as well as to the closing movement of the two members moving together.
- the effect of the force of gravity acting on the lid and seat members 12, 13 will not be constant throughout their pivotal movement. In fact, the force will increase progressively as the lid/seat members 12, 13 pivot from their initial generally upright position towards their lower, generally horizontal position.
- the assembly will be tailored to accommodate this variable force. This can be achieved in the assembly here by suitably configuring the profile of the ramped surfaces 34a, 34b on the driving elements 30a, 30b.
- the amount of resistive damping force that the damper 17 generates is basically proportional to the rate of its axial compression: a higher rate of compression produces a larger damped resistive force and vice versa.
- ramped surfaces 34a, 34b on the driving elements 30a, 30b follow a plain helical pattern, this will produce a constant amount of linear displacement of the end caps 21a, 21b per degree of rotation of the driving elements, i.e. a constant rate of axial compression of the damper 17. If the ramped surfaces 34a, 34b are instead configured to have an increasingly steep profile beyond helical, then this will cause an increasingly rapid rate of axial compression of the damper 17 per degree of rotation of the driving elements 30a, 30b.
- the damped resistive force from the assembly can thus be matched to the variable load from the lid/seat members.
- the profiling of the ramped surfaces 34a, 34b can also be configured to determine the precise range of rotational movement of the lid and seat members 12, 13 during which the damper is to provide damped resistance. For example, it might typically be preferred for there to be no damping force during the first 20° of the initial rotational movement of the lid and seat members from their upright position towards their lower position. In that case, each ramped surface 34a, 34b would be configured with an initial section of its profile lying normal to the hinge axis 20.
- the assembly will normally be designed not to impart any damping force to oppose the opening movement of the seat and lid members upwardly from their lower position.
- the damper may incorporate a valve mechanism in its piston.
- damper it is not essential for the damper to incorporate a spring: an alternative mechanism could be provided for urging the damper towards its extended position.
- the free end of the piston rod could be attached to the surface against which it is arranged to act.
- the damper could be augmented by one or more additional dampers mounted in parallel.
- the assembly could be designed to accommodate two separate dampers aligned along the pivotal axis.
- the dampers could be arranged to react against a common fixed point in the assembly, for example in the form of a central wall within the block.
- Each of the dampers would then separately serve a respective one of the seat and lid members.
- FIG 4 shows a second form of damped hinge assembly, again for use on a lavatory seat 11 comprising a lid member 12 and a seat member 13, both of which are pivotally mounted onto a lavatory 14.
- the pivotal mounting of the lid and seat members 12, 13 comprises a pair of separate mounting units 50a, 50b.
- the mounting units 50a, 50b are anchored to the lavatory 14 by means of threaded fasteners 16 located in the usual spaced apart mounting holes.
- the mounting units 50a, 50b are essentially identical and each comprises a block 51a, 5 lb (shown partly cut away) which is effectively fixed to the lavatory 14. In each block 51a, 51b there is mounted a hinge damper unit 52.
- each hinge damper unit 52 together provide a dual function: firstly, they provide a pivotal mounting for the lid and seat elements 12, 13 and secondly, they provide a resistive damping force to their closing movement.
- the construction of each hinge damper unit 52 is seen in more detail in Figures 5 and 6 and consists of a housing 53, a damper 54 and a drive cap 55. At one end the housing 53 has an externally splined section 56 by which it can be mounted to the block 51a, 51b: this holds the housing non- rotatably fixed to the block. At its other end the housing 53 has a plain cylindrical surface 57: this acts as a spindle for the pivotal mounting of one of the lid and seat elements 12, 13.
- the housing 53 is closed off at one end by a wall 58.
- the drive cap 55 is mounted at the other end of the housing 53.
- the drive cap 55 is mounted so as to be rotatable relative to the housing 53, but is flanged (as at 59) so as to be retained axially in position relative to the housing.
- the drive cap 55 is provided with splines 60.
- the drive cap 55 acts as a pivotal mounting for the other of the lid and seat elements 12, 13.
- the splines 60 on the drive cap 55 ensure that the connection between the two is non-rotatable, ie when the lid or seat element to which it is connected is pivoted, it will cause a corresponding rotational movement of the drive cap 55.
- the drive cap 55 On its interior, the drive cap 55 is provided with a pair of diametrically opposed keyways 61.
- the damper 54 here is again of the linear piston and cylinder variety, with a piston (not shown) connected to a piston rod 62 and acting within a cylinder 63 on a damping medium such as silicone, and with a spring (not shown) biassing the piston rod towards its extended position.
- the free end of the piston rod 62 is arranged to abut against the end wall 58 of the housing 53.
- the spring is again not essential here and the piston rod 62 could be attached to the end wall 58 of the housing 53.
- the cylinder 63 has a specially shaped external profile. At its end opposite its piston rod 62, it has a pair of diametrically opposed keys 64.
- the keys 64 are designed to engage the key ways 61 of the drive cap 55.
- the cylinder 63 also comprises a pair of diametrically opposed ribs 65, each extending around its outer surface. Each rib 65 is shaped with a camming profile that is designed to engage with a respective one of a pair of diametrically opposed lugs 66 provided on the interior of the housing 53. The ribs 65 and their respective lugs 66 cooperate together in the manner of a cam and cam follower and act to convert rotational movement of the drive cap 55 into axial displacement of the cylinder 63.
- the damper 54 will be designed to produce a damped restrictive force on contraction, but no resistance on extension (it may incorporate a valve in its piston for this purpose).
- the assembly can be set up to provide a damped resistive force to the pivotal closing movement of the lid/seat element, without resistance to its opening movement.
- the assembly is arranged so that the hinge damper unit in one of the blocks will provide damping for one of the lid and seat elements, whilst the hinge damper unit in the other block will provide damping for the other element. It will be noted that this conveniently does not require the hinge damper unit to be separately handed: the same device can be used in each case.
- this form of assembly can be designed to produce a tailored damped resistive force.
- the nature of the rib/lug engagement between the cylinder 63 and housing 53 is designed to allow for the possibility of varying the camming profile. With a strictly helical camming profile, for example, this would produce a constant amount of axial displacement of the cylinder 63 per degree of rotation of the drive cap 55. If the camming profile is designed to increase progressively from the helical, then this would produce an increasing amount of axial displacement per degree of rotation. Also, the starting point of the camming profile could be adjusted in order to delay the onset of the axial displacement until after a certain amount of rotation. Other variations of the camming profile are of course possible to allow a wide range of different solutions tailored to suit different applications.
- the motion converting mechanism described above could be embodied in a number of different ways.
- the camming profile could instead be provided in the form of grooves or cut- aways formed in the surface of the cylinder.
- An example of this alternative form is seen in Figure 7.
- a pair of diametrically opposed rebates 70 is formed in the outer surface of the cylinder 63.
- the housing 53 here is formed with a pair of diametrically opposed lugs 71 which extend into its interior and engage complementarily with respective rebates.
- the various cam and cam follower formations described above which act as the movement converting mechanisms could equally well be provided the other way round on their respective components.
- the profiled rebates of the Figure 7 example could be provided on the housing, rather than on the cylinder, with the lugs in that case being provided on the cylinder, rather than on the housing.
- the assemblies described above are suitable for use in other applications, including for example in vertical alignment for hanging doors. In that case, the assemblies could be used in the manner of a rising butt hinge and provide damping to the movement of the door as it falls and closes under the force of gravity. Alternatively, the assemblies could be used in the manner of a normal swinging hinge and provide a damped resistive force to the closing movement of the door.
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- Health & Medical Sciences (AREA)
- Public Health (AREA)
- Pivots And Pivotal Connections (AREA)
Abstract
A damped hinge assembly is provided for mounting a first member (12, 13) for pivotal movement relative to a second member (14) about an axis of rotation (20). The assembly comprises a linear damper (17), which is mounted with its longitudinal axis parallel to the hinge axis, and a cam drive arrangement (21a, 21b, 30a, 30b) for converting the pivotal movement of the first member in at least one direction of rotation into linear displacement of the damper. This causes the damper to produce a damped resistive force to counter the pivotal movement of the first member. The longitudinal axis of the damper is arranged to be coincident with the hinge axis.
Description
Improvements in damped hinge assemblies
This invention relates to damped hinge assemblies and more particularly, though not exclusively, to damped hinge assemblies for mounting elements such as lids, seats and doors.
The invention provides a damped hinge assembly for mounting a first member for pivotal movement relative to a second member about an axis of rotation, the assembly comprising a linear damper, means mounting the damper with its longitudinal axis parallel to the hinge axis, and camming means for converting pivotal movement of the first member in at least one direction of rotation into linear displacement of the damper to cause the damper to produce a damped resistive force to counter said pivotal movement of the first member, wherein the longitudinal axis of the damper is arranged to be coincident with the hinge axis.
By way of example, embodiments ol the invention will now be described with reference to the accompanying drawings, in which:
Figure 1 shows a first form of damped hinge assembly according to the invention (shown partly cut-away to reveal detail),
Figure 2 is a detail view of the drive mechanism of the assembly of Figure 1,
Figure 3 is an exploded view of the Figure 2 detail,
Figure 4 shows a second form of damped hinge assembly according to the invention (shown partly cut-away to reveal detail),
Figures 5 and 6 show in partly cut-away detail the damping unit of the assembly of Figure 4, and
Firgure 7 shows in partly cut-away detail an alternative form of damping unit for the assembly of Figure 4.
The damped hinge assembly seen in Figure 1 is for use on a lavatory seat 11. The seat 11 comprises a lid member 12 and a seat member 13, both of which are pivotally mounted onto the lavatory 14 by means of a hinge mounted on a block 22 (shown partly cut away in the drawings). The block 22 is anchored to the lavatory 14 by means of the usual spaced apart threaded fasteners 16. The arrangement enables both the lid and seat members 12, 13 to be pivotable between a lower, generally horizontal position resting on the lavatory 14 and a raised position, generally slightly beyond vertical and resting against a cistern or wall or the like. The assembly is arranged to provide a damped resistive force to counter the pivotal movement of both the lid and seat members 12, 13 as they move under gravity from their raised position to their lowered position. This is intended to avoid possible damage that could otherwise occur if the lid and/or seat members were accidentally allowed to fall freely onto the lavatory.
The assembly comprises a damper 17, which is conveniently located in the space between the hinge block mounting fasteners 16. The damper 17 here is a linear damper of the piston and cylinder variety, with a piston (not shown) connected to a piston rod 18 and acting within a cylinder 19 on a damping medium (not shown) such as silicone (see Figure 3). The damper 17 incorporates a spring (not shown) arranged to bias the piston rod 18 towards its extended position. The damper 17 is designed here to provide the damped resistive force-to the lid and/or seat members 12, 13 in response to its axial compression. However, the damper 17 provides no damped resistance upon its axial extension.
As will be seen in the drawings, the damper 17 is mounted on the block 22 and arranged with its longitudinal axis coincident with the pivotal axis 20 of the assembly. The damper 17 is captured in this position between two spaced apart end caps 21a, 21b. Each end cap 21a, 21b is generally cylindrical and has an axially extending rib 23a, 23b which engages in a groove 24 in the block 22. The groove 24 extends parallel to the pivotal axis 20 of the assembly. The arrangement means that the two end caps 21a, 21b are both capable of linear movement parallel to the pivotal axis 20 of the assembly (both towards and away from each other), but are prevented from rotating relative to the block 22. Thus, movement of the end caps 21a, 21b towards each other will cause axial compression of the damper 17, whilst movement of the end caps 21a, 21b away from each other will allow axial extension of the damper, under the influence of its spring.
As will be seen in the drawings, the lid and seat members 12, 13 each have a respective driving element 30a, 30b associated therewith. Each driving element 30a, 30b is rotatably mounted on the assembly by means of a spindle 3 la, 3 lb journalled in a bore in the block 22. The axis of rotation of the spindles 31a, 31b is coincident with the pivotal axis 20 of the assembly. Each driving element 30a, 30b is arranged to be keyed to its respective lid/seat member 12, 13 so as to rotate therewith. In the case of the lid member 12, for example, it can be seen in the drawings how the spindle 31a of its respective driving element 30a is provided with flats 37a and fits in a flatted hole 36 in the hinge part of the lid member. The arrangement means that whenever the lid member 12 is pivoted, the spindle 31a and hence its associated driving element 30a will likewise be driven to rotate. In a similar manner, the spindle 31b is provided with flats 37b and fits in a flatted hole in the hinge part of the seat member 13 so that whenever the seat member is pivoted, the spindle 31b and hence its associated driving element 30b will likewise be driven to rotate.
Each driving element 30a, 30b has circumferentially extending ramped surfaces 34a, 34b on its axially inwardly facing end. For balance, the ramped surfaces are provided on their elements as diametrically opposed pairs, as can be seen in the case of the driving element 30b for the seat member in Figure 3. Each of these ramped surfaces 34a, 34b is engaged by a respective nib 35a, 35b on the end caps 21a, 21b (again provided as diametrically opposed pairs). The nibs 35a, 35b will be biassed into engagement with their respective ramped surfaces 34a, 34b by the action of the spring in the damper 17. It will be understood that this arrangement means that when either of the driving elements 30a, 30b rotates, its ramped surface 34a, 34b will act on the respective nib 35a, 35b to cause longitudinal displacement of its respective end cap 21a, 21b. The ramped surfaces 34a, 34b and nibs 35a, 35b thus act in the manner of a cam and cam follower, translating rotational movement into linear movement. The rotational movement of the lid and/or seat members 12, 13 is thus translated by this motion converting mechanism into linear displacement (extension or compression) of the damper 17. In Figure 2, for example, the assembly is seen in its condition when the lid member is in its raised position, whilst the seat member is in its lower position. The driving element 30b associated with the seat member has been rotated in the direction of arrow A as the seat member has lowered. This has driven its associated end cap 21b in the direction of arrow B by the camming action of the ramped surface 34b on the nib 35b. Movement of the end cap 21b in this manner has caused compression of the damper 17, thereby imparting a damped resistive force to the lowering movement of the seat member. It will be understood that the manner of engagement of the nibs
35a, 35b on their respective ramped surfaces 34a, 34b needs to be capable of
sliding contact. This can be achieved by conveniently making the components of the assembly of moulded plastics material. It will also be understood that the nibs 35a, 35b engage their respective ramped surfaces 34a, 34b over a discrete and relatively small contact area. This allows the possibility for the profile of the ramped surfaces 34a, 34b to be configured in an almost infinite variety of different ways in order to suit different requirements.
Here, the ramped surfaces 34a, 34b on the driving elements 30a, 30b are configured such that pivotal movement of the lid and/or seat members 12, 13 in their lowering direction will cause linear movement of the end caps 21a, 21b in a direction towards each other. The effect of this will be to cause axial compression of the damper 17. Axial compression of the damper 17 will in turn create a resistive damping force which is transmitted back through the drive mechanism to .the lid and/or seat members 12, 13 and hence attenuate their closing movement.
It will be noted that the damper 17 will be actuated to provide a damped resistive force to the closing movement of the lid or seat members 12, 13 moving singly, as well as to the closing movement of the two members moving together.
The effect of the force of gravity acting on the lid and seat members 12, 13 will not be constant throughout their pivotal movement. In fact, the force will increase progressively as the lid/seat members 12, 13 pivot from their initial generally upright position towards their lower, generally horizontal position. Ideally, the assembly will be tailored to accommodate this variable force. This can be achieved in the assembly here by suitably configuring the profile of the ramped surfaces 34a, 34b on the driving elements 30a, 30b. The amount of resistive damping force that the damper 17 generates is basically proportional to the rate of its axial compression: a
higher rate of compression produces a larger damped resistive force and vice versa. If the ramped surfaces 34a, 34b on the driving elements 30a, 30b follow a plain helical pattern, this will produce a constant amount of linear displacement of the end caps 21a, 21b per degree of rotation of the driving elements, i.e. a constant rate of axial compression of the damper 17. If the ramped surfaces 34a, 34b are instead configured to have an increasingly steep profile beyond helical, then this will cause an increasingly rapid rate of axial compression of the damper 17 per degree of rotation of the driving elements 30a, 30b. The damped resistive force from the assembly can thus be matched to the variable load from the lid/seat members.
The profiling of the ramped surfaces 34a, 34b can also be configured to determine the precise range of rotational movement of the lid and seat members 12, 13 during which the damper is to provide damped resistance. For example, it might typically be preferred for there to be no damping force during the first 20° of the initial rotational movement of the lid and seat members from their upright position towards their lower position. In that case, each ramped surface 34a, 34b would be configured with an initial section of its profile lying normal to the hinge axis 20.
The assembly will normally be designed not to impart any damping force to oppose the opening movement of the seat and lid members upwardly from their lower position. For this purpose, the damper may incorporate a valve mechanism in its piston.
It is not essential for the damper to incorporate a spring: an alternative mechanism could be provided for urging the damper towards its extended position. In one example, the free end of the piston rod could be attached to the surface against which it is arranged to act.
In the assembly described above, although the damper is conveniently located within it, there is nevertheless enough room to fit in a unit with a sizeable damping capacity. If necessary, however, the damper could be augmented by one or more additional dampers mounted in parallel.
In a modified arrangement, the assembly could be designed to accommodate two separate dampers aligned along the pivotal axis. In that case, the dampers could be arranged to react against a common fixed point in the assembly, for example in the form of a central wall within the block. Each of the dampers would then separately serve a respective one of the seat and lid members. An advantage of this arrangement would be that the members will be able to experience the same level of damping force regardless of whether they are lowered separately or together. In the arrangement with just a single damper, the effect of the damping force will be less if the seat and lid members are lowered together than if they are lowered individually.
Figure 4 shows a second form of damped hinge assembly, again for use on a lavatory seat 11 comprising a lid member 12 and a seat member 13, both of which are pivotally mounted onto a lavatory 14. In this case, the pivotal mounting of the lid and seat members 12, 13 comprises a pair of separate mounting units 50a, 50b. The mounting units 50a, 50b are anchored to the lavatory 14 by means of threaded fasteners 16 located in the usual spaced apart mounting holes. The mounting units 50a, 50b are essentially identical and each comprises a block 51a, 5 lb (shown partly cut away) which is effectively fixed to the lavatory 14. In each block 51a, 51b there is mounted a hinge damper unit 52. As will be explained in more detail, the pair of hinge damper units 52 together provide a dual function: firstly, they provide a pivotal mounting for the lid and seat elements 12, 13 and secondly, they provide a resistive damping force to their closing movement.
The construction of each hinge damper unit 52 is seen in more detail in Figures 5 and 6 and consists of a housing 53, a damper 54 and a drive cap 55. At one end the housing 53 has an externally splined section 56 by which it can be mounted to the block 51a, 51b: this holds the housing non- rotatably fixed to the block. At its other end the housing 53 has a plain cylindrical surface 57: this acts as a spindle for the pivotal mounting of one of the lid and seat elements 12, 13. The housing 53 is closed off at one end by a wall 58. At the other end of the housing 53, the drive cap 55 is mounted. The drive cap 55 is mounted so as to be rotatable relative to the housing 53, but is flanged (as at 59) so as to be retained axially in position relative to the housing. On its external surface, the drive cap 55 is provided with splines 60. The drive cap 55 acts as a pivotal mounting for the other of the lid and seat elements 12, 13. The splines 60 on the drive cap 55 ensure that the connection between the two is non-rotatable, ie when the lid or seat element to which it is connected is pivoted, it will cause a corresponding rotational movement of the drive cap 55. On its interior, the drive cap 55 is provided with a pair of diametrically opposed keyways 61.
The damper 54 here is again of the linear piston and cylinder variety, with a piston (not shown) connected to a piston rod 62 and acting within a cylinder 63 on a damping medium such as silicone, and with a spring (not shown) biassing the piston rod towards its extended position. The free end of the piston rod 62 is arranged to abut against the end wall 58 of the housing 53. The spring is again not essential here and the piston rod 62 could be attached to the end wall 58 of the housing 53. The cylinder 63 has a specially shaped external profile. At its end opposite its piston rod 62, it has a pair of diametrically opposed keys 64. The
keys 64 are designed to engage the key ways 61 of the drive cap 55. This ensures that the cylinder 63 and drive cap 55 will rotate together, whilst allowing relative axial movement between the two. The cylinder 63 also comprises a pair of diametrically opposed ribs 65, each extending around its outer surface. Each rib 65 is shaped with a camming profile that is designed to engage with a respective one of a pair of diametrically opposed lugs 66 provided on the interior of the housing 53. The ribs 65 and their respective lugs 66 cooperate together in the manner of a cam and cam follower and act to convert rotational movement of the drive cap 55 into axial displacement of the cylinder 63. With the piston rod 62 abutting against the end wall 58 of the housing 53, axial displacement of the cylinder 63 will cause extension or contraction of the damper 54. Preferably, the damper 54 will be designed to produce a damped restrictive force on contraction, but no resistance on extension (it may incorporate a valve in its piston for this purpose). Thus the assembly can be set up to provide a damped resistive force to the pivotal closing movement of the lid/seat element, without resistance to its opening movement.
The assembly is arranged so that the hinge damper unit in one of the blocks will provide damping for one of the lid and seat elements, whilst the hinge damper unit in the other block will provide damping for the other element. It will be noted that this conveniently does not require the hinge damper unit to be separately handed: the same device can be used in each case.
As with the form of assembly previously described, this form of assembly can be designed to produce a tailored damped resistive force. In particular, the nature of the rib/lug engagement between the cylinder 63 and housing 53 is designed to allow for the possibility of varying the camming
profile. With a strictly helical camming profile, for example, this would produce a constant amount of axial displacement of the cylinder 63 per degree of rotation of the drive cap 55. If the camming profile is designed to increase progressively from the helical, then this would produce an increasing amount of axial displacement per degree of rotation. Also, the starting point of the camming profile could be adjusted in order to delay the onset of the axial displacement until after a certain amount of rotation. Other variations of the camming profile are of course possible to allow a wide range of different solutions tailored to suit different applications.
The motion converting mechanism described above could be embodied in a number of different ways. For example, rather than using the form of external ribs extending out from the surface of the cylinder 63, the camming profile could instead be provided in the form of grooves or cut- aways formed in the surface of the cylinder. An example of this alternative form is seen in Figure 7. Here, a pair of diametrically opposed rebates 70 is formed in the outer surface of the cylinder 63. The housing 53 here is formed with a pair of diametrically opposed lugs 71 which extend into its interior and engage complementarily with respective rebates. By carefully profiling the shape of the rebates 70, the arrangement can be designed to produce the desired amount of movement conversion to produce damped resistance tailored to suit movement of the lid/seat elements.
It will be understood that the various cam and cam follower formations described above which act as the movement converting mechanisms could equally well be provided the other way round on their respective components. For example, the profiled rebates of the Figure 7 example could be provided on the housing, rather than on the cylinder, with the lugs in that case being provided on the cylinder, rather than on the housing.
It will be appreciated that the assemblies described above are suitable for use in other applications, including for example in vertical alignment for hanging doors. In that case, the assemblies could be used in the manner of a rising butt hinge and provide damping to the movement of the door as it falls and closes under the force of gravity. Alternatively, the assemblies could be used in the manner of a normal swinging hinge and provide a damped resistive force to the closing movement of the door.
Claims
Claims
A damped hinge assembly for mounting a first member for pivotal movement relative to a second member about an axis of rotation, the assembly comprising a linear damper, means mounting the damper with its longitudinal axis parallel to the hinge axis, and camming means for converting pivotal movement of the first member in at least one direction of rotation into linear displacement of the damper to cause the damper to produce a damped resistive force to counter said pivotal movement of the first member, wherein the longitudinal axis of the damper is arranged to be coincident with the hinge axis.
A hinge assembly as claimed in claim 1 wherein the camming means is configured to produce a varying amount of axial displacement of the damper per degree of pivotal movement of the first member.
A hinge assembly as claimed in claim 1 or claim 2 wherein the camming means is configured to produce intermittent or non- continuous axial displacement of the damper over the range of pivotal movement of the first member.
A hinge assembly as claimed in claim 1, claim 2 or claim 3 wherein the camming means comprises a cam associated with one of the members and a cam follower associated with the other of the members.
A hinge assembly as claimed in claim 4 wherein one of the cam and cam follower is capable of rotational movement about the hinge axis whilst the other is prevented from rotating.
1
6. A hinge assembly as claimed in claim 5 wherein the cam comprises a circumferentially extending camming surface on an axial face of a first driver element.
A hinge assembly as claimed in claim 6 wherein the cam follower comprises a nib on an axial face of a second driver element.
A hinge assembly as claimed in claim 7 wherein each of the camming surface and nib are provided on their respective elements in the form of diametrically opposed pairs.
9. A hinge assembly as claimed in claim 7 or claim 8 wherein one of the driver elements is connected to the first member for rotation therewith, whilst the other driver element is held non-rotatably.
10. A hinge assembly as claimed in claim 9 wherein the non-rotatably held driver element is capable of axial movement parallel to the hinge axis.
11. A hinge assembly as claimed in any preceding claim wherein the assembly is attached to the second member by means of two spaced apart fasteners, with the damper located in the space therebetween.
12. A hinge assembly as claimed in any preceding claim wherein the assembly further mounts a third member for pivotal movement relative to the second member, with the damper arranged to produce a damped resistive force to counter pivotal movement of the third member in at least said one direction of rotation. 13. A hinge assembly as claimed in claim 12 and further comprising a third driver element associated with the third member.
2
14. A hinge assembly as claimed in claim 13 wherein the first and third driver elements are arranged to act on the damper in opposite directions along the hinge axis.
15. A hinge assembly as claimed in any preceding claim wherein the damper is a linear compression damper.
16. A hinge assembly as claimed in claim 15 wherein the damper comprises a spring biasing the damper towards its extended condition.
17. A hinge assembly as claimed in claim 15 or claim 16 and further comprising a second linear compression damper arranged parallel to the longitudinal axis of the first.
18. A hinge assembly as claimed in claim 17 wherein the second damper is arranged with its longitudinal axis coincident with the longitudinal axis of the first.
19. A hinge assembly as claimed in claim 18 wherein each of the first and second dampers are arranged to react against a fixed point and provide damping for a respective one of the seat and lid members.
20. A hinge assembly as claimed in claim 19 wherein the first and second dampers are arranged to react against a common fixed point within the assembly.
21. A hinge assembly as claimed in any one of claims 1 to 5 wherein the cam comprises a camming surface on a circumferential surface of a first driver element.
3
22. A hinge assembly as claimed in claim 21 wherein the cam follower comprises a nib on a circumferential surface of a second driver element.
23. A hinge assembly as claimed in claim 22 wherein each of the camming surface and nib are provided on their respective elements in the form of diametrically opposed pairs.
24. A hinge assembly as claimed in claim 23 wherein one of the camming surface and nib is provided on the damper itself.
25. A lid and/or seat mounted by means of a damped hinge assembly as claimed in any preceding claim.
26. A door mounted by means of a damped hinge assembly as claimed in any one of claims 1 to 24.
27. A door as claimed in claim 24 wherein the damped hinge assembly is arranged to mount the door in the manner of a rising butt hinge.
4
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP11760513.9A EP2606193A1 (en) | 2010-08-19 | 2011-08-19 | Improvements in damped hinge assemblies |
US13/817,566 US9414724B2 (en) | 2010-08-19 | 2011-08-19 | Damped hinge assemblies |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1013919.4 | 2010-08-19 | ||
GBGB1013919.4A GB201013919D0 (en) | 2010-08-19 | 2010-08-19 | Improvements in damped hinge assemblies |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2012022946A1 true WO2012022946A1 (en) | 2012-02-23 |
Family
ID=42984381
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/GB2011/001249 WO2012022946A1 (en) | 2010-08-19 | 2011-08-19 | Improvements in damped hinge assemblies |
Country Status (4)
Country | Link |
---|---|
US (1) | US9414724B2 (en) |
EP (1) | EP2606193A1 (en) |
GB (1) | GB201013919D0 (en) |
WO (1) | WO2012022946A1 (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2015067663A1 (en) * | 2013-11-05 | 2015-05-14 | Lama D. D. Dekani | Hinge assembly |
CN104989202A (en) * | 2015-06-18 | 2015-10-21 | 宁波一扬建材科技有限公司 | Slow-falling hinge |
GB2511480B (en) * | 2012-12-18 | 2017-11-08 | Titus D O O Dekani | Damper assembly |
Families Citing this family (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
TWM444022U (en) * | 2012-08-23 | 2012-12-21 | Dexin Corp | Cover-raisable electronic apparatus |
JP6446718B2 (en) * | 2013-12-27 | 2019-01-09 | 下西技研工業株式会社 | Toilet lid hinges and toilet equipment |
CN103844988B (en) * | 2014-03-21 | 2016-02-10 | 厦门豪帝卫浴工业有限公司 | The upright mechanism for assembling-disassembling of a kind of lavatory lid button-free |
JP1537351S (en) * | 2015-03-13 | 2015-11-09 | ||
JP1537350S (en) * | 2015-03-13 | 2015-11-09 | ||
US11148830B2 (en) | 2017-08-04 | 2021-10-19 | Rocket Lab Usa, Inc. | Satellite deployer with composite guide rail |
GB2571105A (en) * | 2018-02-16 | 2019-08-21 | Titus D O O Dekani | Improvements in damped hinge assemblies |
DE102019132130A1 (en) * | 2019-11-27 | 2021-05-27 | Duravit Aktiengesellschaft | Articulated arrangement for the pivotable mounting of a cover, a seat or a seat-cover set on a ceramic sanitary item |
CA3172850A1 (en) * | 2020-05-11 | 2021-11-18 | Brolock Pty Ltd | A hinge |
IT202000031124A1 (en) * | 2020-12-16 | 2022-06-16 | Nuova Star Spa | HINGE FOR APPLIANCES LID |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3722114A1 (en) * | 1986-07-05 | 1988-01-14 | Nifco Inc | Rotation-damping device |
EP0422882A1 (en) * | 1989-10-11 | 1991-04-17 | Sugatsune Industrial Co., Ltd. | Door hinge |
US5996132A (en) * | 1997-01-24 | 1999-12-07 | Katoh Electrical Machinery Co., Ltd. | Compound torque hinge |
GB2406879A (en) * | 2003-10-09 | 2005-04-13 | Graham Chesworth | Hinge |
US20060230573A1 (en) * | 2005-02-22 | 2006-10-19 | Kao Ching C | Door closing hinge device |
EP2182156A1 (en) * | 2008-10-29 | 2010-05-05 | NEXTER Systems | Device for damping a door of a military vehicle |
Family Cites Families (20)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1993625A (en) * | 1933-02-24 | 1935-03-05 | Riemer Gottfried | Combined hinge and check |
US2474164A (en) * | 1946-01-19 | 1949-06-21 | Riemer George | Check swing hinge |
US5222260A (en) * | 1991-07-01 | 1993-06-29 | Piper Dean E | Toilet cover closure device |
US5279000A (en) * | 1992-11-12 | 1994-01-18 | Mercier William H | Automatic toilet seat lowering hinge assembly |
US5267356A (en) * | 1992-12-10 | 1993-12-07 | Gideon William W | Commode seat lowering apparatus |
US5604936A (en) * | 1995-09-28 | 1997-02-25 | Mausolf; Melvin J. | Self-lowering toilet seat |
JPH10248756A (en) * | 1997-03-14 | 1998-09-22 | Kato Electrical Mach Co Ltd | Hinge for opening and closing for toilet seat and toilet lid of western-style toilet |
JPH10248757A (en) * | 1997-03-14 | 1998-09-22 | Kato Electrical Mach Co Ltd | Hinge for opening and closing toilet seat and toilet lid of western style toilet |
JP3732651B2 (en) * | 1998-04-16 | 2006-01-05 | 加藤電機株式会社 | Opening / closing hinge |
US6275999B1 (en) * | 1998-05-01 | 2001-08-21 | Katoh Electrical Machinery Co., Ltd. | Hinge device for supporting seat and seat lid of toilet bowl openably and closably |
US6393624B1 (en) * | 1998-11-05 | 2002-05-28 | Sankyo Seiki Mfg. Co., Ltd. | Damping device for a toilet seat and lid unit in western-style toilet |
JP2000170813A (en) * | 1998-12-07 | 2000-06-23 | Sugatsune Ind Co Ltd | Rotary damper |
DE10051805B4 (en) * | 2000-10-18 | 2005-04-14 | Hamberger Industriewerke Gmbh | Toilet seat hinge |
US6634033B2 (en) * | 2000-10-30 | 2003-10-21 | Sugatsune Kogyo Co., Ltd. | Rotating damper |
US7377500B2 (en) * | 2003-12-26 | 2008-05-27 | Nifco Inc. | Shock absorbing device for moving body |
WO2008089761A1 (en) * | 2007-01-24 | 2008-07-31 | Pressalit Group A/S | Self-closing mechanism |
EP2208912A1 (en) * | 2007-10-05 | 2010-07-21 | Sugatsune Kogyo CO., LTD. | Hinge device |
US8214932B2 (en) * | 2009-02-11 | 2012-07-10 | Smart Lid, Llc | Automatic self-closing toilet seat assembly |
KR100937780B1 (en) * | 2009-06-08 | 2010-01-20 | 주식회사 삼홍테크 | Oil damper to used cam |
US8307503B1 (en) * | 2009-10-02 | 2012-11-13 | George Burger | Slow closing hinge apparatus |
-
2010
- 2010-08-19 GB GBGB1013919.4A patent/GB201013919D0/en not_active Ceased
-
2011
- 2011-08-19 WO PCT/GB2011/001249 patent/WO2012022946A1/en active Application Filing
- 2011-08-19 US US13/817,566 patent/US9414724B2/en not_active Expired - Fee Related
- 2011-08-19 EP EP11760513.9A patent/EP2606193A1/en not_active Withdrawn
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3722114A1 (en) * | 1986-07-05 | 1988-01-14 | Nifco Inc | Rotation-damping device |
EP0422882A1 (en) * | 1989-10-11 | 1991-04-17 | Sugatsune Industrial Co., Ltd. | Door hinge |
US5996132A (en) * | 1997-01-24 | 1999-12-07 | Katoh Electrical Machinery Co., Ltd. | Compound torque hinge |
GB2406879A (en) * | 2003-10-09 | 2005-04-13 | Graham Chesworth | Hinge |
US20060230573A1 (en) * | 2005-02-22 | 2006-10-19 | Kao Ching C | Door closing hinge device |
EP2182156A1 (en) * | 2008-10-29 | 2010-05-05 | NEXTER Systems | Device for damping a door of a military vehicle |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2511480B (en) * | 2012-12-18 | 2017-11-08 | Titus D O O Dekani | Damper assembly |
WO2015067663A1 (en) * | 2013-11-05 | 2015-05-14 | Lama D. D. Dekani | Hinge assembly |
CN104989202A (en) * | 2015-06-18 | 2015-10-21 | 宁波一扬建材科技有限公司 | Slow-falling hinge |
Also Published As
Publication number | Publication date |
---|---|
US9414724B2 (en) | 2016-08-16 |
GB201013919D0 (en) | 2010-10-06 |
EP2606193A1 (en) | 2013-06-26 |
US20130283568A1 (en) | 2013-10-31 |
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